# TCDS P13NE: Hamilton Standard Division - Type: Type certificate data sheet - Status: Current - Holder: Hamilton Standard Division - Revision: 4 - Revised: August 12, 1996 - Product: Propeller - Certification basis: Part 35 - Data sheet PDF: https://openairdocs.org/files/sha256/39/48/3948bbb87cd95b47bc32bab69c925e93d4260728c999d1c6cfbe8379b7fa62a4 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B097DD8BD8398D2B8525670F0066812B.0001 - Page: https://openairdocs.org/tcds/P13NE ## Models (2) As the data sheet lists them. - 6/5500/F-1 - 6/5500/F-2 ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text * PAGE 1 2 3 REV 4 4 4 ENGINE AND PROPELLER DIRECTORATE FEDERAL AVIATION ADMINISTRATION U.S. DEPARTMENT OF TRANSPORTATION TYPE CERTIFICATE DATA SHEET P13NE TCDS NUMBER P13NE HAMILTON STANDARD REVISION NUMBER: 4 REVISION DATE: AUGUST 12, 1996 MODEL/S: 6/5500/F-1 6/5500/F-2 Propellers of models described herein conforming with this data sheet (which is part of Type Certificate Number P13NE) and other approved data on file with the Federal Aviation Administration, meet the minimum standards for use in certificated aircraft in accordance with pertinent aircraft data sheets and applicable portions of the Federal Aviation Regulations provided they are installed, operated, and maintained as prescribed by the approved manufacturer's manuals and other approved instructions. TYPE CERTIFICATE (TC) HOLDER Hamilton Standard Division United Technologies Corporation 1 Hamilton Road Windsor Locks, CT 06096-1010 TYPE Constant speed; hydraulic (See Notes 3 and 4) ENGINE FLANGE 6.750" Bolt Circle HUB MATERIAL Steel BLADE MATERIAL: Fiberglass covered aluminum spar. NUMBER OF BLADES Six DESIGN SERIES 6/5500/F-1 (RIGHT-HAND), 6/5500/F-2 (LEFT-HAND) BLADE MODELS RIGHT / LEFT MAXIMUM CONTINUOUS SHP RPM SHP RPM APPROXIMATE WEIGHT / LB. UFB14B1-3A / UFB14B2-3A 2380 1200 2670 1200 13'-9" 413.0 UFB14C1-3A / UFB14C2-3A 2380 1200 2670 1200 13'-9" 413.0 UFB14E1-3A / UFB14E2-3A 2380 1200 2670 1200 13'-9" 413.0 UFB14G1-3A / UFB14G2-3A 2380 1200 2670 1200 13'-9" 413.0 CERTIFICATION BASIS: FAR 35 Amendment 5 dated September 11, 1980. TC APPLICATION DATE:: 04/26/84 TC ISSUED: 02/24/87 PRODUCTION BASIS: Production Certificate No. 14 P13NE 2 NOTES NOTE 1: HUB MODEL DESIGNATION: 6 / 5500 / F - 1 F denotes flange mounting Blade shank size Number of blades Indicates a specific model designation which defines a complete propeller assembly, including spinner. NOTE 2. BLADE MODEL DESIGNATION F B 14 B 1 - 3 A Blade spinner interface Normal reduction from basic diameter in inches Structural and operational features (may indicate particular deicing assembly) Basic diameter feet. (Diameter limit shown is nominal diameter of assembled propeller and does not include Major aerodynamic characteristics Denotes fiberglass blade Hamilton Standard shank size U the +1/4-inch / -3/16-inch manufacturing tolerance permissible.) Special notation - See Note 13 Direction of rotation and tip configuration NOTE 3: PITCH CONTROL: Propeller control is specified on the approved model parts list. NOTE 4: (a) FEATHERING: (b) REVERSING: Full feathering with the approved propeller control is specified on approved model parts list. Full reversing with the approved propeller control is specified on approved model parts list. NOTE 5: LEFT-HAND MODELS: The left-hand version of an approved propeller model is eligible at the same rating and diameter limitations as listed for the right-hand model. 3 P13NE NOTE 6: INTERCHANGEABLE BLADES: Not applicable. NOTE 7: ACCESSORIES: (a) Propeller deicing: The electrical deicing system is specified on approved model parts list and installed in accordance with the propeller manufacturer's instructions. (b) Spinners: The spinner is specified on approved model parts list. NOTE 8: SHANK FAIRINGS: Not applicable. NOTE 9: SPECIAL LIMITS: Airworthiness limitations are specified in System Maintenance Manual P5190. NOTE 10: LIFE-LIMITED PARTS: See Note 9. NOTE 11: BLADES: The UFB14B1-3A, UFB14C1-3A, UFB14E1-3A, and UFB14G1-3A blades are approved for use with the model 6/5500/F-1 propeller in sets of six. The left hand versions of these blades are approved for use with the model 6/5500/F-2 propeller in sets of six. NOTE 12: SPECIAL NOTES: Aircraft installations must be approved as part of the aircraft type certification and demonstrate compliance with the applicable airworthiness requirements. NOTE 13: SPECIAL NOTATION: This position of the blade model designation normally consists of a hyphen. This hyphen is replaced by a letter to designate a special characteristic. The meaning of these letters is identified below. “P” is used to identify a blade that “as produced or manufactured” met specific requirements. “R” is used to identify a blade that has been reworked to meet specific requirements. .....END..... ``` ## ADs (12, in force first) - [AD 2013-16-10](https://openairdocs.org/ad/2013-16-10): Inspections · Hamilton Standard Division 24PF-303, 24PF-304, 24PF-305 and 41 more. Effective Sep 19, 2013 - [AD 96-25-20](https://openairdocs.org/ad/96-25-20): Transfer Tube Assemblies · Hamilton Standard Division 6/5500/F-1, 6/5500/F-2, 14RF-19 and 10 more. Effective Feb 7, 1997 - [AD 96-08-02](https://openairdocs.org/ad/96-08-02): Blades · Hamilton Standard Division 6/5500/F-1, 6/5500/F-2, 14RF-19 and 10 more. Effective May 9, 1996 - [AD 95-22-12](https://openairdocs.org/ad/95-22-12): Control Unit Servo Ballscrew Internal Spline Assembly · Hamilton Standard Division 6/5500/F-1, 6/5500/F-2, 14RF-19 and 12 more. Effective Nov 24, 1995 - [AD 93-06-06](https://openairdocs.org/ad/93-06-06): Control Unit Ballscrew · Hamilton Standard Division 6/5500/F-1, 14RF-19, 14RF-21 and 8 more. Effective Jul 6, 1993 - [AD 96-01-01](https://openairdocs.org/ad/96-01-01) (historical): Blade Taper Bore · Hamilton Standard Division 14RF-19, 14RF-21, 14RF-9 and 9 more. Effective Jan 19, 1996 - [AD 95-05-03](https://openairdocs.org/ad/95-05-03) (historical): Blade · Hamilton Standard Division 14RF-19, 14RF-21, 14RF-9 and 10 more. Effective Mar 23, 1995 - [AD 94-09-06](https://openairdocs.org/ad/94-09-06) (historical): Blade Taper Bore · Hamilton Standard Division 14RF-19, 14RF-21, 14RF-9 and 9 more. Effective May 2, 1994 - [AD 95-18-06 PL](https://openairdocs.org/ad/95-18-06-PL) (historical): Blade Taper Bore · Hamilton Standard Division 14RF-19, 14RF-21, 14RF-9 and 9 more - [AD 95-18-06 R1](https://openairdocs.org/ad/95-18-06-R1) (historical): Blade Taper Bore · Hamilton Standard Division 14RF-19, 14RF-21, 14RF-9 and 9 more - [AD T91-11-51](https://openairdocs.org/ad/T91-11-51) (historical): Loss of control of the propeller system · Hamilton Standard Division 6/5500/F-1, 14RF-19, 14RF-21 and 5 more - [AD T95-18-51](https://openairdocs.org/ad/T95-18-51) (historical): Blade Taper Bore · Hamilton Standard Division 14RF-19, 14RF-21, 14RF-9 and 9 more --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.